CA2124343C - Recoverable fabric sleeve - Google Patents
Recoverable fabric sleeve Download PDFInfo
- Publication number
- CA2124343C CA2124343C CA 2124343 CA2124343A CA2124343C CA 2124343 C CA2124343 C CA 2124343C CA 2124343 CA2124343 CA 2124343 CA 2124343 A CA2124343 A CA 2124343A CA 2124343 C CA2124343 C CA 2124343C
- Authority
- CA
- Canada
- Prior art keywords
- sleeve
- fibres
- fabric
- heat recoverable
- heat
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C61/00—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
- B29C61/06—Making preforms having internal stresses, e.g. plastic memory
- B29C61/0608—Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms
- B29C61/0658—Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms consisting of fibrous plastics material, e.g. woven
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C61/00—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
- B29C61/06—Making preforms having internal stresses, e.g. plastic memory
- B29C61/0608—Making preforms having internal stresses, e.g. plastic memory characterised by the configuration or structure of the preforms
- B29C61/0633—Preforms comprising reinforcing elements
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/53—Joining single elements to tubular articles, hollow articles or bars
- B29C66/532—Joining single elements to the wall of tubular articles, hollow articles or bars
- B29C66/5326—Joining single elements to the wall of tubular articles, hollow articles or bars said single elements being substantially flat
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7371—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable
- B29C66/73715—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable heat-shrinkable
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- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D1/00—Woven fabrics designed to make specified articles
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- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D1/00—Woven fabrics designed to make specified articles
- D03D1/0035—Protective fabrics
- D03D1/0043—Protective fabrics for elongated members, i.e. sleeves
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G15/00—Cable fittings
- H02G15/08—Cable junctions
- H02G15/18—Cable junctions protected by sleeves, e.g. for communication cable
- H02G15/1806—Heat shrinkable sleeves
- H02G15/1813—Wraparound or slotted sleeves
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C61/00—Shaping by liberation of internal stresses; Making preforms having internal stresses; Apparatus therefor
- B29C61/06—Making preforms having internal stresses, e.g. plastic memory
- B29C61/10—Making preforms having internal stresses, e.g. plastic memory by bending plates or sheets
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/60—Riveting or staking
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/62—Stitching
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/24—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight
- B29C66/242—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours
- B29C66/2422—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being circular, oval or elliptical
- B29C66/24221—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being closed or non-straight said joint lines being closed, i.e. forming closed contours being circular, oval or elliptical being circular
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/729—Textile or other fibrous material made from plastics
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/73—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/737—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined
- B29C66/7371—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable
- B29C66/73711—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the state of the material of the parts to be joined oriented or heat-shrinkable oriented
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S428/00—Stock material or miscellaneous articles
- Y10S428/913—Material designed to be responsive to temperature, light, moisture
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
- Y10T428/1362—Textile, fabric, cloth, or pile containing [e.g., web, net, woven, knitted, mesh, nonwoven, matted, etc.]
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/30—Woven fabric [i.e., woven strand or strip material]
- Y10T442/3179—Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
- Y10T442/322—Warp differs from weft
- Y10T442/3228—Materials differ
- Y10T442/3236—Including inorganic strand material
- Y10T442/3252—Including synthetic polymeric strand material
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Textile Engineering (AREA)
- Woven Fabrics (AREA)
- Laminated Bodies (AREA)
- Materials For Medical Uses (AREA)
- Undergarments, Swaddling Clothes, Handkerchiefs Or Underwear Materials (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
- Protection Of Pipes Against Damage, Friction, And Corrosion (AREA)
Abstract
A heat recoverable sleeve has a high recovery ratio of at least 60 %. It uses a specific arrangement of recoverable fibres in one direction woven in a twill configuration with both heat stable fibres and heat recoverable fibres extending in another direc-tion.
Description
~~Vi) 93/1292 - I - PGTlG~92/02351 Recoverable fabric Sleeve This invention relates to a heat recoverable fabric sleeve for enclosing an elongate object such as a pipe or cable, or a joint between pipes or cables. In particular the invention relates to such a sleeve for covering an: object which varies in cross-sectional area along~fs~ength.
Heat recoverable articles are well known. They are articles whose dimensional configuration may be made to change when subjected to an appropriate treatment. Typically heat recoverable articles comprise a heat shrinkable sleeve made from a polymeric anaterial that exhibits the property of elastic or plastic nnemory as described, for example in LJS
patents 2027962, 3086242 and 3597372: More recently heat recoverable articles a~mprisiatg fabrics have become known, as described for exaanple in EP-A-OII6393 (MP0790): E~'-A-OI:I7026 (RICI76), EP-~-OI 15905 (RKI77) and EP-A-0116392 (RKI78). These comprise a recoverable fabric in conjunction with a polymeric matrix formed by laminating a polymeric a~~terial to one or both sides of 'the fabric t~ render it impervious.
Recoverable fabrics' have found may applications. EP'-~-Ol 15905 describes a polymeric-larninat~d, heat recoverable fabric~having a recovery ratio bf at'leasx 400; preferably at least 50 or 60% that array be used for example t~ cover sbbstrates with varyPing or discontinuous coast~~ars to provide inechax~ical pr~tection or pr~tection from the environment. Tie entire disclosure of ~-B-0115905 is incorporated herein by referenee.
Within the scope of the invention desr~abed in EP-B-0125905 we have dies~verecl a specific heat recoverable fabric configa~ratioa~ that grovides a high recovery ratio and particularly advantageo~xs properties.
A first as~aect of the invention provides a heat 'recoverable sleeve havang a recovery ratio of at least 60% preferably at least 70%, and coinpriSin~:
.-..5 ..u. , .. .. ., u..... .... .... . ' . , . ~ . . ...~. ... ....n. . ,.". , . , ..,. ....'..h .e.m...,-...... n... .. ,...., v 1... . , . ,. ' 'W~ 93/12921 _ 2 _ P~.'1'1~~92/02351 (a) a woven fabric having 10 to 20 heat recoverable fibres per cm extending in one direction, woven in a twill, preferably a broken twill, configuration with 1-10 heat stable fibres per cm in the other weave direction, and 1-~ heat recoverable fibres per cm in the said other weave direction, and (b) polymeric ynaterial laminated to at least one side of the,fabric. .
The recovery ratio in the present invention is defined in terms of percentages. The ratio represents a change in a dimension as a percentage of the same dimension before recovery. The recovery ratio of the present invention is preferably at least 6p%, more preferably at least ~0%. patios as high as 75% or even 7~ or g0% array even be achieved. This large recovery ratio allows the sleeve to be used inter alia in applications where the elongate object exhibits large transitions in cross-sectional area.
The heat recoverable sleeve is preferably heat-shrinkable, preferably radially.
exaynples of applicati~ns; the sleeve may be used t~ cover pipes or cabhs ~r jbi~ts therebetween: Particaular ~pplic~ta~ns include (i) end saps for distrihea~ang pipes where one end of the sleeve needs t~ recover onto the outer thick insulation; ansi the other end needs to recover onto the much sanaller diameter steel pipe, (ii) eo~ers for mechanical or flange couplers f~r pipes, ah.d (iii) covers f~x bell and spigot joints bett~veen pipes.
In such, appliea~aord~ the ~axiachuan rrds~-sectional dimension of the object to be covered gay be as much 3s5 tune, or even 4.5 times the mixiiaa~u~ dimension of the objesctt' to be covered. A, sleeve of the present invents~n that is initially ~f unif~rm cross-seed~nal sire along its length can advantageously ~e made to shrink around these substrates exhibiting large changes in diixnensions' al~ng their length.
.~e have f~uncl that the fabric design is an important parameter in aehievin~ a high recc~~rery rati~ fabric: In partic~zlar we have found a broken till 2/4 design is the n~~st effective. The configurati~~n of a broken will 2/~ design is described later with reference to the drawings.
TWO 93!12921 _ 3 _ PGT/GB92/0235a The sleeve rxiay be woven in a closed tubular configuration (ie, a sleeve of closed cross-section), but is preferably a wraparound sleeve, longitudinal edges of which can be held together to hold the sleeve in a closed configuration before recovery. As an example, overlapping longitudinal edges of the wrapped sleeve array be fixed to each other by a mechanical joining arrangement that penetrates the fabric, eg stitching, stapling or riveting. As another example a patch (which may~itself include a fabric which may or may not be the same design as the sleeve, a.nd may or may not be heat recoverable) may be secured to one longitudinal edge of the sleeve. The securement of the patch may be by a mechanical joining arrangement that penetrates that patch and the longitudinal sleeve edge, or by adhesive. Thus; in a preferred embodiment, at least one longitudinal edge of the sleeve is penetrated by a mechanical joining arrangement, preferably stitching, stapling or riveting, which joins that edge (t) to the other longitudinal edge or (ii) to a patch, in order to close the sleeve.
141eehanical penetrating arrangements for joining heat-recoverable fabric sleeves are described in EP 1~-OI37648 (RK205? the entire disclosure of w~~ is ; incorporated herein by reference. , Where one edge of a patch is secured ;to the sleeve, the patch is preferably adhesiv~coated and the adhesive used to close the wraparound sleeve diuring installation.
~~ r~v,~able fabric may be provided by defornvng a fabric woven f~roxn diutensional stable fibres. It may also be provided by interlinking. (preferably weaving) fibres that are already recoverable. The fibres rnay be cross-linked and then stretched to render thenn recoverable.
The fibres may, instead; be initially stretched and then doss-linked during the weaving process. Cross=linking may be achieved by irradiation with a beam of !ugh energy electrodes, by chemical cross-linking reactions, or using silane-technology.
The formed fabric is laminated on at least one, prefferably on at least both sides with a polymeric material which can be a thermoplastic or an ela~tom~: Suitable examples include ethylene vinyl/acetate copolymers, WO 93/12921 _ 4 _ PGT/GB9Z/02351 ~t ethyl acrylate copolymers, polyethylenes including linear low, low density and high density polyethylene, acrylonitrile butadiene styrene block copolymers, and acrylic elastomers. Other example are mentioned , in EP-B-0115905 (RlEGG177) and EP-A- 0116393 (MP0790COM) ~, Preferably the polymeric material extends throughout the recoverable fabric. Preferably a true composite structure is formed between the recoverable fabric and the polymeric material. This is described in EP-A-0116393.
~~t The laminated fabric may then be subjected to cross-linking. As before the cross-linking may be achieved by irradiation by a beam of high energy electrons, by chemical cross-linking, or using silane technology.
The irradiation step cross-links both the recoverable fibres of the fabric and the matrix polymer, and is additional to any initial cross-linking applied to render the fibres heat recoverable.
For a heat recoverable fabric comprising recoverable fibres we can speak of unresolved recoveay stress of the fibres and the fabric. This is the stress exertable by the fabric as'a whole or by the individual fibres on recovery: 'This recovery stress can be given, for example, for 100%
unresolved recovery (ie before any recovery has 'taken place) or for X%
unresolved recovery ie where (I00 - 7C)% of the recovery available has heady taken place: This unresolved recovery stress influences the recovery force of the Fibres and the fabric, and also the resistance of the fibres (and hence also the fabric) to splitting on recovery of the sleeve.
We have found that for our fabric sleeve it is desirable for the unresolved recovery stress of the fabric, for 100% unresolved recovery (ie where no recovery has taken place) ~ be in the region of 13N/SOmm to 21~T/50n~n (0.185 MPa to 0.3 MPa). 'I'hhe yninimum value as important substantially td grevent fibre melting; and also to provide that when the sleeve is recovered into contact with a substrate; there is some remaining residual recovery force. 'l hhe residual force (i) ensures good contact is maintained with the substrate, even after cooling; and (ii) where the sleeve is ec~ated with adhesive or sealant, urges that adhesive or sealant into sealing contact with the substrate. The maximum value minimises ~plitiing. .~4lso the unresolved recovery stress exerts hoop forces at the closure region of a wraparound sleeve. Depending on the type of closure 2~~~~ ~4J
WO 93!12921 - 5 - PCTlGB92l02351 used it may be advantageous to minimise the recovery force of the fabric, so that the hoop forces acting on the closure are liznited. Therefore, for some applications, for example, where an adhesive bonded patch is used to close the wraparound sleeve, it is desirable to restrict the recovery force of the fabric to less than 21N/50mm. This reduces the tendency of the patch to shear relative to the wrapped sleeve.
Sianilarly the unresolved recovery stress of the fabric at 30%
unresolved recovery (ie 70% actual recovery) is preferably at least 1N/50n1m (0.0142 lVlha) (plus the effect of the weight of the sleeve). This manimurn recovery stress is as explained above particularly desirable for a heat shrinkable sleeve lined with an adhesive, or particularly if lined with a sealant such as a mastic, since it provides sufficient force to urge the adhesive or sealant down against the object to be covered. For many applications large masses of sealant are positioned on the object, eg around a pipe joint, and this needs to be pushed against by the sleeve in order to form an effective ffinished sealed joint. This is achieved by the minimum unresolved recovery stress of 1N/50mzzt at 30% unresolved recovery, and the minimum recovery stress of 13I~T/50mnn at 100% unresolved recovery.
~~nsadering the fibres making up the fabric; the unresolved recovery sta°ess of the fibres (at 100% unresolved recovery) is preferably in the range of O.1N/fibre to 0.2N/fibres (for fibres of 0.4mm diameter, that is x 10"~ N/Tex to Z5 x 10''f N/Tex. A Tex is the weight in g per crn.
The fabric design of the present invention is advantageously ~~~~ ~ a~eve the above desr~ibed unresolved recovery stresses in addition t~ tie lzi~h ~reeovery ratao of at least ~0% preferably at least 70%, or wen as high as 75, 78 or g0%. This therefore allows a combination of re~very over large transitions while exerting relatively low hoop stresses at a closure of a wraparound sleeve. This unique combination is a particularly advantage of the fabric design of the present invention.
The fibres xnay be rendered heat recoverable (cg by cross-linking and then deforming the fibres) before or after they are made into a fabric. This initial cross-linking of the fibres step influences the unresolved recovery stress ~f the fibres referred to above. Also as mentioned above, a second W~ 93/12921 - 6 - PCI'/GB92/02351 cross-linking step may be carried out after lamination. This influences the behaviour of the matrix as well as the sleeve, as is described fully in EP-B-OlIC393 (R/IP0790COM EP) and EP-B-0115905 (RIC177).
The sleeve comprises 10-20 heat recoverable fibres in one direction.
This provides the predominant recovery direction of the sleeve, and thus is arranged preferably to extend in the circunlferential directiqn of the sleeve. The predominant recovery direction may constitute 'either the warp or the weft of the fabric. For some applications, particularly where large diameter sleeves are required, at preferably constitutes the warp, enabling large sleeves to be made on reasonable sized machines. Sleeves up to 150 em or even 300 cm in diameter can be made in this way.
Preferably the heat recoverable fibres are 0.3-0.5mm, especially about 0.4mm in diameter. Preferably the heat recoverable fibres have a Tex (weight in g per rm) of 50 to 200. Each recoverable fibre may comprise, for example, a shrinkable polyethylene fibre. The fibres preferably have a tensile strength of at least 0.1 Il/ti'~ at their recovery temperature.
The fibres may be m~n~filaments, mufti-filaneents, spun staple yarns or yarns produced by fibrillation (cg from film). The recovery temperature of the fibres is preferably 100-150°C.
The sleeve comprises l-l0 heaf stable tibres/cm in the other direction, preferably the length df section, ~f the sleeve. A preferred material for th~se fibres i~ glues. Preferably 6 fibres/cm are included cg 3 pairs / cue.. The heat stablo ffbr~s can (i) enlanc~e the burst strength of the sleeve, cg in ~pglications where the slave is subjeet to internal pressure aid (ii) determiaae the axial strength of the sleeve.
Preferably the sleeve comprises up to 4, preferably 1.to 2, especially I.S heat recoverable fibres per can in the other direction, preferably the lera~th direction, of the sleeve; in addition to those in the first (preferably ~.a~al) direction of the sleeve. The purpose of these is to achieve ~, sms~oth surface after recovery.
In one embodimQnt the fabric according to the invention includes a .. ~: ...,., .
T-:!
. .4 ../. ~~
:-:;~ .. ..
,'.'i -.:.... , , ~:. f . ~) :~...' . . ~.~ . !.~ ''~n. .,... ..;.i. .'.-'"~ .
.. '.'.~ a..~~:u. .... r a. . .:.~~.~
au.u .. , .......... _...,.. ,t.. .. .,. . .:~_ ..... .. ._... .. _. .. . u., . ,. . .
< <
s~ R )~ ~
~~.~'~c3 J
'i~~ 93/12921 - 7 - PC.TI~~92t02351 heating wire for supplying heat to effect recovery. The wire is_preferably arranged in a zig zag configuration with the main length of the wires extending along the length of the sleeve. This is described in EP-,A- .
0258519 (B100C~OM EPC).
The sleeve may be lined with an adhesive or sealant. Instead, or in addition, an inner sealing sleeve whieh is wholly made of adhyesive or sealant, or which is lined with adhesive or sealant may be us~d.~
The invention is now described by way of example with reference to the accompanying drawings wherein:
Figs 1 arid 2 are schematic drawings of a fabric design ('broken twill 2/4) according to the invention . Figure 1 is a block diagram as used in the fabrication industry. The 6 by b square block illustrates the passage of 6 adjacent fibres in each of the warp and the weft. In the diagram the weft extends horizontally and the ~w~rp vertically. A white square illustrates a fibre passing over the fibre in the other direction. this is also illustrated in the more literal diagram Figure 2. In Figwres I and 2 the heat-stable or non-recoverable glass fibres are referenced 1 and the heat shrinkable pe,~~emyleaae Bbres are ref~rer~ced 2. If will be seen that in the wreft (reprinted 'by the hdrizr~ntal raves in Figure 1) the heat-stable glass fibre gasses over ft9ur fibres ~aad then under two fibres; ~erhile the polyethylene fibres pass over t~nro fibres and then under one. In the warp (the vertical colunvns) the heat recoverable fibres pass veer four fibres and tlyn under o. In eaeh case where four fiibres are passed over, the portion of the fibres parsed ovea.° is staggered i.~ adjacent row~ and also in adjacent colta~nns Figs 3a and 3b sh~~VS a fabric sleeve according to the invention positlone~ around a district heating pipe end before and after xecovery.
°I°he ~iastrict heating pipe coanpresses an inner steel pipe 4 and an outer i~m~tion and covering layer 6 which is cut back at its end to bare the steel pipe. ~°here ;s a sharp transiBon 8 at the end of the cut back insulation b, which needs to be covered. A heat recoverable, wraparound fabric sleeve of broken twill 2/4 design as illustrated in Figures 1 and 2 is positioned over the transition. A heat stable paten 12 is stitched to one longitudinal . . , ..:. . :... . .. ,;. . ..... : ,~:.:~:., .. -:- -:. . -- , ,: ,::. . .
,. .
... . . .... .... . . , . . . . . ".. ,.. . , -.. . ... ... . . . .
y . ~ h r; r '.'f..
~~~~~~~J
'F,r,,.
W~ 93/12921 - g - PC'I'/G8921023~3 edge of the sleeve 10. The patch is secured .to the underlying sleeve to close the wraparound. This securement can be by adhesive or by a mechanical closure. I-ieat is then applaed to recover the sleeve. The recovered edges (now designated 10') is shown in contact with the pipe covering the sharp transition in Figure 2. ' The Following example is given to illustrate a wraparound .built from preferred materials.
Exara~~le The following 1-IDPIJ monofilament was chosen to provide the recoverable coanponent, l~rln ~ number average molecular weight 29,400 Mw = weight average molecular weight 120,800 lVlp -- peak molecular weight 57,500 I) _ Ie~h,Jlkin polydispersity 4.I
Initial R~Iodulus (IvIPa) . 3881.3 Tensile Strength (tea) 534.4 % Elortg~titoxt (21 C) Zl 1lrlon~fila~ent dia () 0.38 This fibre h~ the fallowing properties:
Fibre Properties IZacliation Dosage (l~iaads) Pro er 0 8 16 32 100% odulus (lViPa) O.I3 ' 0.3 0.42 Tensile Strength 0.93 1.4 1.46 El~ngatioh ~to Break (%) 1,480 924 754 gel ~on~e~t (%) 27.0 58.0 67.0 Itecwea~y Force (lVIPa) 1.17 1.2 1.3 Recovery (%) 98 96 95 ~~.'?~~: ~~
liVO 9/92929 ~ ~ - ~'C.'9'11aB92102359 The HDPE fibres were woven with non-recoverable glass fibres to produce the fabric design illustrated in Figure 1. The recoverable HDPE
fibres were the only fibres in the warp. Recoverable HI~PE fibres and glass were in the weft.
The glass fibres are preferably ones having the designation EC 9 34 tex x 25152. 'This type of designation is standard and will be ~dTerstood by those in the art. Briefly it has the following meaning EC refers to the tex value of the bundles of filaments, x 2S refers to the number of monofilaanents in the bundle, 152 refers to the I52 twists in the bundles per metre.
The warp density was I5 ends/cm, and the weft density was about 4.4 per can (3 glass bundles and 1.5 HDPE in a 2 glass bundles: 1 HDPE
repeating pattern). Hence the warp was the predominant shrink direction.
The fabric was rendered substantially impervious by laminating to it a low density polyethylene at a thickness of 0.5 mm on both sides.
~,~nir:ation eras carried out at such a temperature, pressure and pracessing speed that tine material permeated the interstices of the fabric but no recovex°yy ~ccurred.
1'he resulting composite was subjected to an irradiation step with 16 rrleV electsons in air at rdba~ temperature for times sufficient to produce the required a°ecovery rati~
°~e exulting coa~nposite material had a recovery of at least 70%'0.
'The c~mposite ~natex°ial was used to produce a wraparound sleeve suitable for~use for covering a pipe in conjunction with a closure patch.
The ~lave was arranged with the predonvinant shrink direction around the circumference.
'tee cognposite material was coated .with a hot-melt adhesive on that side snrhieh would be inwardly facing when the sleeve was in the q ". ... ... . ,. :, ,. ,. , ,.; . . : ., 7. .
.... _.:. ..,~ ~"~:~ ,;..~., ;'... .~':'~ ., '.": .,.., ;;: , ...,,;. . , .,..,. .... ~~ ...,:~ . .. ..' .. ..::.,'. . '"~ .'.'.
,. ,, : ~ . . :.. . , . :~ :. . -, , , . , ~ ~~.~. . :. . . , ~. .," ~...,.. , : ~.. .. . . . ... . :: .~.... r... . .. . :. ; . ... .. . .. .
t~ ~ t~
~'.,.vr>
~!'~ 93/12921 - t~ - PCY'JG~92J02351 ~~ r wrapped around corafiguratioz~. The adhesive used was a~piied to a thickness of 1.2 mram
Heat recoverable articles are well known. They are articles whose dimensional configuration may be made to change when subjected to an appropriate treatment. Typically heat recoverable articles comprise a heat shrinkable sleeve made from a polymeric anaterial that exhibits the property of elastic or plastic nnemory as described, for example in LJS
patents 2027962, 3086242 and 3597372: More recently heat recoverable articles a~mprisiatg fabrics have become known, as described for exaanple in EP-A-OII6393 (MP0790): E~'-A-OI:I7026 (RICI76), EP-~-OI 15905 (RKI77) and EP-A-0116392 (RKI78). These comprise a recoverable fabric in conjunction with a polymeric matrix formed by laminating a polymeric a~~terial to one or both sides of 'the fabric t~ render it impervious.
Recoverable fabrics' have found may applications. EP'-~-Ol 15905 describes a polymeric-larninat~d, heat recoverable fabric~having a recovery ratio bf at'leasx 400; preferably at least 50 or 60% that array be used for example t~ cover sbbstrates with varyPing or discontinuous coast~~ars to provide inechax~ical pr~tection or pr~tection from the environment. Tie entire disclosure of ~-B-0115905 is incorporated herein by referenee.
Within the scope of the invention desr~abed in EP-B-0125905 we have dies~verecl a specific heat recoverable fabric configa~ratioa~ that grovides a high recovery ratio and particularly advantageo~xs properties.
A first as~aect of the invention provides a heat 'recoverable sleeve havang a recovery ratio of at least 60% preferably at least 70%, and coinpriSin~:
.-..5 ..u. , .. .. ., u..... .... .... . ' . , . ~ . . ...~. ... ....n. . ,.". , . , ..,. ....'..h .e.m...,-...... n... .. ,...., v 1... . , . ,. ' 'W~ 93/12921 _ 2 _ P~.'1'1~~92/02351 (a) a woven fabric having 10 to 20 heat recoverable fibres per cm extending in one direction, woven in a twill, preferably a broken twill, configuration with 1-10 heat stable fibres per cm in the other weave direction, and 1-~ heat recoverable fibres per cm in the said other weave direction, and (b) polymeric ynaterial laminated to at least one side of the,fabric. .
The recovery ratio in the present invention is defined in terms of percentages. The ratio represents a change in a dimension as a percentage of the same dimension before recovery. The recovery ratio of the present invention is preferably at least 6p%, more preferably at least ~0%. patios as high as 75% or even 7~ or g0% array even be achieved. This large recovery ratio allows the sleeve to be used inter alia in applications where the elongate object exhibits large transitions in cross-sectional area.
The heat recoverable sleeve is preferably heat-shrinkable, preferably radially.
exaynples of applicati~ns; the sleeve may be used t~ cover pipes or cabhs ~r jbi~ts therebetween: Particaular ~pplic~ta~ns include (i) end saps for distrihea~ang pipes where one end of the sleeve needs t~ recover onto the outer thick insulation; ansi the other end needs to recover onto the much sanaller diameter steel pipe, (ii) eo~ers for mechanical or flange couplers f~r pipes, ah.d (iii) covers f~x bell and spigot joints bett~veen pipes.
In such, appliea~aord~ the ~axiachuan rrds~-sectional dimension of the object to be covered gay be as much 3s5 tune, or even 4.5 times the mixiiaa~u~ dimension of the objesctt' to be covered. A, sleeve of the present invents~n that is initially ~f unif~rm cross-seed~nal sire along its length can advantageously ~e made to shrink around these substrates exhibiting large changes in diixnensions' al~ng their length.
.~e have f~uncl that the fabric design is an important parameter in aehievin~ a high recc~~rery rati~ fabric: In partic~zlar we have found a broken till 2/4 design is the n~~st effective. The configurati~~n of a broken will 2/~ design is described later with reference to the drawings.
TWO 93!12921 _ 3 _ PGT/GB92/0235a The sleeve rxiay be woven in a closed tubular configuration (ie, a sleeve of closed cross-section), but is preferably a wraparound sleeve, longitudinal edges of which can be held together to hold the sleeve in a closed configuration before recovery. As an example, overlapping longitudinal edges of the wrapped sleeve array be fixed to each other by a mechanical joining arrangement that penetrates the fabric, eg stitching, stapling or riveting. As another example a patch (which may~itself include a fabric which may or may not be the same design as the sleeve, a.nd may or may not be heat recoverable) may be secured to one longitudinal edge of the sleeve. The securement of the patch may be by a mechanical joining arrangement that penetrates that patch and the longitudinal sleeve edge, or by adhesive. Thus; in a preferred embodiment, at least one longitudinal edge of the sleeve is penetrated by a mechanical joining arrangement, preferably stitching, stapling or riveting, which joins that edge (t) to the other longitudinal edge or (ii) to a patch, in order to close the sleeve.
141eehanical penetrating arrangements for joining heat-recoverable fabric sleeves are described in EP 1~-OI37648 (RK205? the entire disclosure of w~~ is ; incorporated herein by reference. , Where one edge of a patch is secured ;to the sleeve, the patch is preferably adhesiv~coated and the adhesive used to close the wraparound sleeve diuring installation.
~~ r~v,~able fabric may be provided by defornvng a fabric woven f~roxn diutensional stable fibres. It may also be provided by interlinking. (preferably weaving) fibres that are already recoverable. The fibres rnay be cross-linked and then stretched to render thenn recoverable.
The fibres may, instead; be initially stretched and then doss-linked during the weaving process. Cross=linking may be achieved by irradiation with a beam of !ugh energy electrodes, by chemical cross-linking reactions, or using silane-technology.
The formed fabric is laminated on at least one, prefferably on at least both sides with a polymeric material which can be a thermoplastic or an ela~tom~: Suitable examples include ethylene vinyl/acetate copolymers, WO 93/12921 _ 4 _ PGT/GB9Z/02351 ~t ethyl acrylate copolymers, polyethylenes including linear low, low density and high density polyethylene, acrylonitrile butadiene styrene block copolymers, and acrylic elastomers. Other example are mentioned , in EP-B-0115905 (RlEGG177) and EP-A- 0116393 (MP0790COM) ~, Preferably the polymeric material extends throughout the recoverable fabric. Preferably a true composite structure is formed between the recoverable fabric and the polymeric material. This is described in EP-A-0116393.
~~t The laminated fabric may then be subjected to cross-linking. As before the cross-linking may be achieved by irradiation by a beam of high energy electrons, by chemical cross-linking, or using silane technology.
The irradiation step cross-links both the recoverable fibres of the fabric and the matrix polymer, and is additional to any initial cross-linking applied to render the fibres heat recoverable.
For a heat recoverable fabric comprising recoverable fibres we can speak of unresolved recoveay stress of the fibres and the fabric. This is the stress exertable by the fabric as'a whole or by the individual fibres on recovery: 'This recovery stress can be given, for example, for 100%
unresolved recovery (ie before any recovery has 'taken place) or for X%
unresolved recovery ie where (I00 - 7C)% of the recovery available has heady taken place: This unresolved recovery stress influences the recovery force of the Fibres and the fabric, and also the resistance of the fibres (and hence also the fabric) to splitting on recovery of the sleeve.
We have found that for our fabric sleeve it is desirable for the unresolved recovery stress of the fabric, for 100% unresolved recovery (ie where no recovery has taken place) ~ be in the region of 13N/SOmm to 21~T/50n~n (0.185 MPa to 0.3 MPa). 'I'hhe yninimum value as important substantially td grevent fibre melting; and also to provide that when the sleeve is recovered into contact with a substrate; there is some remaining residual recovery force. 'l hhe residual force (i) ensures good contact is maintained with the substrate, even after cooling; and (ii) where the sleeve is ec~ated with adhesive or sealant, urges that adhesive or sealant into sealing contact with the substrate. The maximum value minimises ~plitiing. .~4lso the unresolved recovery stress exerts hoop forces at the closure region of a wraparound sleeve. Depending on the type of closure 2~~~~ ~4J
WO 93!12921 - 5 - PCTlGB92l02351 used it may be advantageous to minimise the recovery force of the fabric, so that the hoop forces acting on the closure are liznited. Therefore, for some applications, for example, where an adhesive bonded patch is used to close the wraparound sleeve, it is desirable to restrict the recovery force of the fabric to less than 21N/50mm. This reduces the tendency of the patch to shear relative to the wrapped sleeve.
Sianilarly the unresolved recovery stress of the fabric at 30%
unresolved recovery (ie 70% actual recovery) is preferably at least 1N/50n1m (0.0142 lVlha) (plus the effect of the weight of the sleeve). This manimurn recovery stress is as explained above particularly desirable for a heat shrinkable sleeve lined with an adhesive, or particularly if lined with a sealant such as a mastic, since it provides sufficient force to urge the adhesive or sealant down against the object to be covered. For many applications large masses of sealant are positioned on the object, eg around a pipe joint, and this needs to be pushed against by the sleeve in order to form an effective ffinished sealed joint. This is achieved by the minimum unresolved recovery stress of 1N/50mzzt at 30% unresolved recovery, and the minimum recovery stress of 13I~T/50mnn at 100% unresolved recovery.
~~nsadering the fibres making up the fabric; the unresolved recovery sta°ess of the fibres (at 100% unresolved recovery) is preferably in the range of O.1N/fibre to 0.2N/fibres (for fibres of 0.4mm diameter, that is x 10"~ N/Tex to Z5 x 10''f N/Tex. A Tex is the weight in g per crn.
The fabric design of the present invention is advantageously ~~~~ ~ a~eve the above desr~ibed unresolved recovery stresses in addition t~ tie lzi~h ~reeovery ratao of at least ~0% preferably at least 70%, or wen as high as 75, 78 or g0%. This therefore allows a combination of re~very over large transitions while exerting relatively low hoop stresses at a closure of a wraparound sleeve. This unique combination is a particularly advantage of the fabric design of the present invention.
The fibres xnay be rendered heat recoverable (cg by cross-linking and then deforming the fibres) before or after they are made into a fabric. This initial cross-linking of the fibres step influences the unresolved recovery stress ~f the fibres referred to above. Also as mentioned above, a second W~ 93/12921 - 6 - PCI'/GB92/02351 cross-linking step may be carried out after lamination. This influences the behaviour of the matrix as well as the sleeve, as is described fully in EP-B-OlIC393 (R/IP0790COM EP) and EP-B-0115905 (RIC177).
The sleeve comprises 10-20 heat recoverable fibres in one direction.
This provides the predominant recovery direction of the sleeve, and thus is arranged preferably to extend in the circunlferential directiqn of the sleeve. The predominant recovery direction may constitute 'either the warp or the weft of the fabric. For some applications, particularly where large diameter sleeves are required, at preferably constitutes the warp, enabling large sleeves to be made on reasonable sized machines. Sleeves up to 150 em or even 300 cm in diameter can be made in this way.
Preferably the heat recoverable fibres are 0.3-0.5mm, especially about 0.4mm in diameter. Preferably the heat recoverable fibres have a Tex (weight in g per rm) of 50 to 200. Each recoverable fibre may comprise, for example, a shrinkable polyethylene fibre. The fibres preferably have a tensile strength of at least 0.1 Il/ti'~ at their recovery temperature.
The fibres may be m~n~filaments, mufti-filaneents, spun staple yarns or yarns produced by fibrillation (cg from film). The recovery temperature of the fibres is preferably 100-150°C.
The sleeve comprises l-l0 heaf stable tibres/cm in the other direction, preferably the length df section, ~f the sleeve. A preferred material for th~se fibres i~ glues. Preferably 6 fibres/cm are included cg 3 pairs / cue.. The heat stablo ffbr~s can (i) enlanc~e the burst strength of the sleeve, cg in ~pglications where the slave is subjeet to internal pressure aid (ii) determiaae the axial strength of the sleeve.
Preferably the sleeve comprises up to 4, preferably 1.to 2, especially I.S heat recoverable fibres per can in the other direction, preferably the lera~th direction, of the sleeve; in addition to those in the first (preferably ~.a~al) direction of the sleeve. The purpose of these is to achieve ~, sms~oth surface after recovery.
In one embodimQnt the fabric according to the invention includes a .. ~: ...,., .
T-:!
. .4 ../. ~~
:-:;~ .. ..
,'.'i -.:.... , , ~:. f . ~) :~...' . . ~.~ . !.~ ''~n. .,... ..;.i. .'.-'"~ .
.. '.'.~ a..~~:u. .... r a. . .:.~~.~
au.u .. , .......... _...,.. ,t.. .. .,. . .:~_ ..... .. ._... .. _. .. . u., . ,. . .
< <
s~ R )~ ~
~~.~'~c3 J
'i~~ 93/12921 - 7 - PC.TI~~92t02351 heating wire for supplying heat to effect recovery. The wire is_preferably arranged in a zig zag configuration with the main length of the wires extending along the length of the sleeve. This is described in EP-,A- .
0258519 (B100C~OM EPC).
The sleeve may be lined with an adhesive or sealant. Instead, or in addition, an inner sealing sleeve whieh is wholly made of adhyesive or sealant, or which is lined with adhesive or sealant may be us~d.~
The invention is now described by way of example with reference to the accompanying drawings wherein:
Figs 1 arid 2 are schematic drawings of a fabric design ('broken twill 2/4) according to the invention . Figure 1 is a block diagram as used in the fabrication industry. The 6 by b square block illustrates the passage of 6 adjacent fibres in each of the warp and the weft. In the diagram the weft extends horizontally and the ~w~rp vertically. A white square illustrates a fibre passing over the fibre in the other direction. this is also illustrated in the more literal diagram Figure 2. In Figwres I and 2 the heat-stable or non-recoverable glass fibres are referenced 1 and the heat shrinkable pe,~~emyleaae Bbres are ref~rer~ced 2. If will be seen that in the wreft (reprinted 'by the hdrizr~ntal raves in Figure 1) the heat-stable glass fibre gasses over ft9ur fibres ~aad then under two fibres; ~erhile the polyethylene fibres pass over t~nro fibres and then under one. In the warp (the vertical colunvns) the heat recoverable fibres pass veer four fibres and tlyn under o. In eaeh case where four fiibres are passed over, the portion of the fibres parsed ovea.° is staggered i.~ adjacent row~ and also in adjacent colta~nns Figs 3a and 3b sh~~VS a fabric sleeve according to the invention positlone~ around a district heating pipe end before and after xecovery.
°I°he ~iastrict heating pipe coanpresses an inner steel pipe 4 and an outer i~m~tion and covering layer 6 which is cut back at its end to bare the steel pipe. ~°here ;s a sharp transiBon 8 at the end of the cut back insulation b, which needs to be covered. A heat recoverable, wraparound fabric sleeve of broken twill 2/4 design as illustrated in Figures 1 and 2 is positioned over the transition. A heat stable paten 12 is stitched to one longitudinal . . , ..:. . :... . .. ,;. . ..... : ,~:.:~:., .. -:- -:. . -- , ,: ,::. . .
,. .
... . . .... .... . . , . . . . . ".. ,.. . , -.. . ... ... . . . .
y . ~ h r; r '.'f..
~~~~~~~J
'F,r,,.
W~ 93/12921 - g - PC'I'/G8921023~3 edge of the sleeve 10. The patch is secured .to the underlying sleeve to close the wraparound. This securement can be by adhesive or by a mechanical closure. I-ieat is then applaed to recover the sleeve. The recovered edges (now designated 10') is shown in contact with the pipe covering the sharp transition in Figure 2. ' The Following example is given to illustrate a wraparound .built from preferred materials.
Exara~~le The following 1-IDPIJ monofilament was chosen to provide the recoverable coanponent, l~rln ~ number average molecular weight 29,400 Mw = weight average molecular weight 120,800 lVlp -- peak molecular weight 57,500 I) _ Ie~h,Jlkin polydispersity 4.I
Initial R~Iodulus (IvIPa) . 3881.3 Tensile Strength (tea) 534.4 % Elortg~titoxt (21 C) Zl 1lrlon~fila~ent dia () 0.38 This fibre h~ the fallowing properties:
Fibre Properties IZacliation Dosage (l~iaads) Pro er 0 8 16 32 100% odulus (lViPa) O.I3 ' 0.3 0.42 Tensile Strength 0.93 1.4 1.46 El~ngatioh ~to Break (%) 1,480 924 754 gel ~on~e~t (%) 27.0 58.0 67.0 Itecwea~y Force (lVIPa) 1.17 1.2 1.3 Recovery (%) 98 96 95 ~~.'?~~: ~~
liVO 9/92929 ~ ~ - ~'C.'9'11aB92102359 The HDPE fibres were woven with non-recoverable glass fibres to produce the fabric design illustrated in Figure 1. The recoverable HDPE
fibres were the only fibres in the warp. Recoverable HI~PE fibres and glass were in the weft.
The glass fibres are preferably ones having the designation EC 9 34 tex x 25152. 'This type of designation is standard and will be ~dTerstood by those in the art. Briefly it has the following meaning EC refers to the tex value of the bundles of filaments, x 2S refers to the number of monofilaanents in the bundle, 152 refers to the I52 twists in the bundles per metre.
The warp density was I5 ends/cm, and the weft density was about 4.4 per can (3 glass bundles and 1.5 HDPE in a 2 glass bundles: 1 HDPE
repeating pattern). Hence the warp was the predominant shrink direction.
The fabric was rendered substantially impervious by laminating to it a low density polyethylene at a thickness of 0.5 mm on both sides.
~,~nir:ation eras carried out at such a temperature, pressure and pracessing speed that tine material permeated the interstices of the fabric but no recovex°yy ~ccurred.
1'he resulting composite was subjected to an irradiation step with 16 rrleV electsons in air at rdba~ temperature for times sufficient to produce the required a°ecovery rati~
°~e exulting coa~nposite material had a recovery of at least 70%'0.
'The c~mposite ~natex°ial was used to produce a wraparound sleeve suitable for~use for covering a pipe in conjunction with a closure patch.
The ~lave was arranged with the predonvinant shrink direction around the circumference.
'tee cognposite material was coated .with a hot-melt adhesive on that side snrhieh would be inwardly facing when the sleeve was in the q ". ... ... . ,. :, ,. ,. , ,.; . . : ., 7. .
.... _.:. ..,~ ~"~:~ ,;..~., ;'... .~':'~ ., '.": .,.., ;;: , ...,,;. . , .,..,. .... ~~ ...,:~ . .. ..' .. ..::.,'. . '"~ .'.'.
,. ,, : ~ . . :.. . , . :~ :. . -, , , . , ~ ~~.~. . :. . . , ~. .," ~...,.. , : ~.. .. . . . ... . :: .~.... r... . .. . :. ; . ... .. . .. .
t~ ~ t~
~'.,.vr>
~!'~ 93/12921 - t~ - PCY'JG~92J02351 ~~ r wrapped around corafiguratioz~. The adhesive used was a~piied to a thickness of 1.2 mram
Claims (12)
1. A heat recoverable sleeve having a recovery ratio of at least 60% comprising:
(a) a woven fabric having 10 to 20 heat recoverable fibres per cm extending in one direction, woven in a twill configuration with 1-10 heat stable fibres per cm in the other weave direction, and 1-4 heat recoverable fibres per cm in the said other weave direction, and (b) polymeric material laminated to at least one side of the fabric.
(a) a woven fabric having 10 to 20 heat recoverable fibres per cm extending in one direction, woven in a twill configuration with 1-10 heat stable fibres per cm in the other weave direction, and 1-4 heat recoverable fibres per cm in the said other weave direction, and (b) polymeric material laminated to at least one side of the fabric.
2. A heat recoverable sleeve having a recovery ratio of at least 70% comprising:
(a) a woven fabric having 10 to 20 heat recoverable fibres per cm extending in one direction, woven in a twill configuration with 1-10 heat stable fibres per cm in the other weave direction, and 1-4 heat recoverable fibres per cm in the said other weave direction, and (b) polymeric material laminated to at least one side of the fabric.
(a) a woven fabric having 10 to 20 heat recoverable fibres per cm extending in one direction, woven in a twill configuration with 1-10 heat stable fibres per cm in the other weave direction, and 1-4 heat recoverable fibres per cm in the said other weave direction, and (b) polymeric material laminated to at least one side of the fabric.
3. The heat recoverable sleeve according to claim 1 or 2, wherein the fabric configuration is broken twill 2/4.
4. The heat recoverable sleeve according to any one of claims 1 to 3, wherein the sleeve is a wraparound sleeve.
5. The heat recoverable sleeve according to claim 4, wherein at least one longitudinal edge of the sleeve is penetrated by a mechanical joining arrangement, which joins the at least one edge (i) to another longitudinal edge or (ii) to a patch, in order to close the sleeve.
6. The heat recoverable sleeve according to claim 5, wherein the mechanical joining arrangement is stitching.
7. The heat recoverable sleeve according to claim 5, wherein the mechanical joining arrangement is stapling.
8. The heat recoverable sleeve according to claim 5, wherein the mechanical joining arrangement is riveting.
9. The heat recoverable sleeve according to any one of claims 1 to 8, wherein the fabric has an unresolved recovery stress at 10% unresolved recovery in the range 13N/50mm (0.185 MPa) to 21N/50mm (0.3 MPa).
10. The heat recoverable sleeve according to any one of claims 1 to 9, wherein the fabric has an unresolved recovery stress at 30% unresolved recovery of at least 1N/50mm (0.0142 MPa).
11. The heat recoverable sleeve according to any one of claims 1 to 10, wherein the heat recoverable fibres comprise polyethylene.
12. The heat recoverable sleeve according to claim 11, wherein the heat stable fibres are glass fibres.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9127103.1 | 1991-12-20 | ||
GB9127103A GB9127103D0 (en) | 1991-12-20 | 1991-12-20 | Recoverable fabric sleeve |
PCT/GB1992/002351 WO1993012921A1 (en) | 1991-12-20 | 1992-12-18 | Recoverable fabric sleeve |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2124343A1 CA2124343A1 (en) | 1993-07-08 |
CA2124343C true CA2124343C (en) | 2002-10-29 |
Family
ID=10706621
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA 2124343 Expired - Fee Related CA2124343C (en) | 1991-12-20 | 1992-12-18 | Recoverable fabric sleeve |
Country Status (10)
Country | Link |
---|---|
US (1) | US5527575A (en) |
EP (1) | EP0618860B1 (en) |
JP (1) | JP3222468B2 (en) |
AT (1) | ATE159456T1 (en) |
CA (1) | CA2124343C (en) |
DE (1) | DE69222865T2 (en) |
GB (1) | GB9127103D0 (en) |
IN (1) | IN181106B (en) |
RU (1) | RU2097195C1 (en) |
WO (1) | WO1993012921A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10407807B2 (en) | 2014-09-24 | 2019-09-10 | Federal-Mogul Powertrain Llc | Textile sleeve with adhesive fixation layer and methods of construction and use thereof |
EP4372134A1 (en) * | 2022-11-21 | 2024-05-22 | Tyco Electronics UK Ltd | Heat-shrink fabric tubing and method of constructing a heat-shrink fabric tubing |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2027962A (en) * | 1933-03-03 | 1936-01-14 | Nat Carbon Co Inc | Production of articles from plastic compositions |
NL130678C (en) * | 1960-07-15 | 1900-01-01 | ||
NL270833A (en) * | 1960-10-31 | |||
US3945493A (en) * | 1974-11-13 | 1976-03-23 | The Pillsbury Company | Shrink wrap system for products on pallets and slip sheets |
BR8400031A (en) * | 1983-01-06 | 1984-08-14 | Raychem Ltd | PROCESS OF CLOSING A PROFILED SUBSTRATE, PROCESS OF CLOSING A SEAMLESS, PROCESS OF CLOSING A JOINT, RECOVERABLE ARTICLE AND ELONGED SUBSTRATE |
US4624720A (en) * | 1983-01-06 | 1986-11-25 | Raychem Ltd | Dimensionally heat-recoverable article |
BR8400030A (en) * | 1983-01-06 | 1984-08-14 | Raychem Ltd | RECOVERABLE WRAP ARTICLE, PROCESS OF CLOSING A SUBSTRATE, PROCESS OF FORMING A CLOSING MEMBER AND PROCESS OF FORMING A WRAP SHEET |
IN159633B (en) * | 1983-01-06 | 1987-05-30 | Raychem Corp | |
US4626458A (en) * | 1983-01-06 | 1986-12-02 | Raychem Limited | Recoverable article for encapsulation |
US4631098A (en) * | 1983-01-06 | 1986-12-23 | Raychem Limited | Heat-recoverable article |
GB8322004D0 (en) * | 1983-08-16 | 1983-09-21 | Raychem Ltd | Heat-recoverable article |
ES8607108A1 (en) * | 1984-04-06 | 1986-06-01 | Raychem Sa Nv | Heat-recoverable article. |
GB8625369D0 (en) * | 1986-10-23 | 1986-11-26 | Raychem Ltd | Heat recoverable fabric article |
GB8702833D0 (en) * | 1987-02-09 | 1987-03-18 | Raychem Sa Nv | Recoverable fabric sleeve |
US4952437A (en) * | 1987-07-15 | 1990-08-28 | Firma Rxs Schrumpftechnik-Garnituren Gmbh | Heat-shrinkable sleeve |
US4929477A (en) * | 1987-07-15 | 1990-05-29 | Firma Rxs Schrumpftechnik-Garnituren Gmbh | Heat-shrinkable sleeve and the process for the production thereof |
GB8921967D0 (en) * | 1989-09-29 | 1989-11-15 | Raychem Sa Nv | Recoverable fabric sleeve |
-
1991
- 1991-12-20 GB GB9127103A patent/GB9127103D0/en active Pending
-
1992
- 1992-12-15 IN IN748MA1992 patent/IN181106B/en unknown
- 1992-12-18 DE DE69222865T patent/DE69222865T2/en not_active Expired - Fee Related
- 1992-12-18 US US08/256,063 patent/US5527575A/en not_active Expired - Fee Related
- 1992-12-18 AT AT93900302T patent/ATE159456T1/en not_active IP Right Cessation
- 1992-12-18 JP JP51152193A patent/JP3222468B2/en not_active Expired - Fee Related
- 1992-12-18 WO PCT/GB1992/002351 patent/WO1993012921A1/en active IP Right Grant
- 1992-12-18 EP EP19930900302 patent/EP0618860B1/en not_active Expired - Lifetime
- 1992-12-18 RU RU94041217/25A patent/RU2097195C1/en not_active IP Right Cessation
- 1992-12-18 CA CA 2124343 patent/CA2124343C/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
RU2097195C1 (en) | 1997-11-27 |
JP3222468B2 (en) | 2001-10-29 |
JPH07502466A (en) | 1995-03-16 |
DE69222865D1 (en) | 1997-11-27 |
GB9127103D0 (en) | 1992-02-19 |
US5527575A (en) | 1996-06-18 |
CA2124343A1 (en) | 1993-07-08 |
EP0618860B1 (en) | 1997-10-22 |
RU94041217A (en) | 1996-04-10 |
IN181106B (en) | 1998-04-25 |
WO1993012921A1 (en) | 1993-07-08 |
ATE159456T1 (en) | 1997-11-15 |
DE69222865T2 (en) | 1998-04-30 |
EP0618860A1 (en) | 1994-10-12 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request | ||
MKLA | Lapsed |